View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 68239U 26145.00002315 +.00000000 +00000-0 +57271-4 0 00006
2 68239 53.1583 295.7891 0000709 43.7141 105.5456 15.35402493 04
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0000709 |
| inclination: | 53.1583° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 295.7891° |
| argument of perigee: | 43.7141° |
| revolutions per day: | 15.35402493 |
| mean anomaly at epoch: | 105.5456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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